Abstract
Fatigue lifetime of model AF1410 ultrahigb-strength steel as a function of fatigue hold time (time expended at peak loads) and type and severity of environment is presented. Results indicate significant reduction in lifetime as a function of rising hold time for specimens charged with hydrogen, whereas a parabolic trend was observed in the case of specimens tested in air and in the presence of simulated marine environment Compared with baseline tests in air, a gradual reduction in lifetime was observed as a function of increasing concentration of hydrogen in the specimens. Micrographie, atomic force microscope, and scanning electron microscope analysis is performed to study the various aspects of AF1410 lifetime.
| Original language | English |
|---|---|
| Pages (from-to) | 453-458 |
| Number of pages | 6 |
| Journal | Journal of Aircraft |
| Volume | 44 |
| Issue number | 2 |
| DOIs | |
| State | Published - 2007 |
| Externally published | Yes |
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